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    • 1. 发明申请
    • A METHOD AND NODES FOR PAGING IN A RADIO ACCESS NETWORK
    • 无线接入网络中的寻呼方法和方法
    • WO2014008912A1
    • 2014-01-16
    • PCT/EP2012/063348
    • 2012-07-09
    • TELEFONAKTIEBOLAGET L M ERICSSON (publ)XIA, QiDE WIT, ErikSÖRENSON, LennartSVENSSON, Håkan
    • XIA, QiDE WIT, ErikSÖRENSON, LennartSVENSSON, Håkan
    • H04W68/02
    • H04W68/02H04W24/02H04W68/06
    • The present invention relates to a method for paging a user equipment, UE, in a radio access network, RAN, served by a core network node. When a UE attaches to the radio access network, a service area identity included in the respective a respective registration message from each UE, is received (31) and registered (32) in the core network node. The method further includes a step of receiving (310) one or more data packets to be sent to a receiving UE attached to the network and determining (320) a permitted latency for delivery of the one or more data packets to the UE. When (330) permitted latency exceeds a predetermined latency threshold, a step of retrieving (340) the registered SAI for the receiving UE is performed. In a concluding step in the method of paging, a first page is performed of the UE, directing (350) the first page to cells belonging to a first paging area determined by the retrieved SAI. The present invention also relates to a core network node and a radio access node configured to contribute when carrying enhanced paging procedure.
    • 本发明涉及一种在由核心网络节点服务的无线接入网络RAN中寻呼用户设备的方法。 当UE附接到无线电接入网络时,在核心网络节点中接收(31)并注册(32)在每个UE的各自的注册消息中包括的服务区域身份。 该方法还包括接收(310)要发送给附接到网络的接收UE的一个或多个数据分组的步骤,并确定(320)向UE发送一个或多个数据分组的允许等待时间。 当(330)允许等待时间超过预定等待时间阈值时,执行检索(340)接收UE的注册SAI的步骤。 在寻呼方法的结束步骤中,对UE执行第一页面,将第一页面指向(350)属于由所检索的SAI确定的第一寻呼区域的小区。 本发明还涉及核心网络节点和被配置为在承载增强的寻呼过程时贡献的无线电接入节点。
    • 3. 发明申请
    • DEVICE FOR BRACING A SHELL IN AN AIRCRAFT FUSELAGE
    • 用于在飞机熔接中制造壳体的装置
    • WO2002098733A1
    • 2002-12-12
    • PCT/SE2002/000787
    • 2002-04-23
    • SAAB ABBROFÄLDT, Pär
    • BROFÄLDT, Pär
    • B64C1/06
    • B64C1/12
    • A device for bracing a shell surface (1) in an aircraft fuselage against deformations and consisting of a continuous profile that is arranged so as, after conformation, to be mounted against the shell surface. Notches (6) are spaced at regular distances apart from each other in at least a portion of the profile. The notches (6) extend through a base surface (3) in the profile, and through an intermediate part (4) perpendicular to the base surface (3). The notches (6) are delimited upwardly by an upper surface (5) that is not encompassed by said notches (6).
    • 一种用于支撑飞机机身中的壳体表面(1)的装置,用于防止变形,并且包括连续轮廓,所述连续轮廓在构造之后被布置成抵靠壳体表面安装。 凹槽(6)在轮廓的至少一部分中彼此间隔开规则的距离。 凹口(6)延伸穿过轮廓中的基面(3),并穿过垂直于基面(3)的中间部分(4)。 凹口(6)由不由所述凹口(6)包围的上表面(5)向上限定。
    • 6. 发明申请
    • REFLECTOR AND ANTENNA SYSTEM CONTAINING REFLECTORS
    • 包含反射器的反射器和天线系统
    • WO2002061882A1
    • 2002-08-08
    • PCT/SE2002/000188
    • 2002-02-02
    • SAAB ERICSSON SPACE ABPETERSSON, MikaelINGVARSON, Per
    • PETERSSON, MikaelINGVARSON, Per
    • H01Q15/22
    • H01Q3/2658H01Q15/22H01Q19/12H01Q19/195H01Q21/28H01Q25/001H01Q25/007
    • The invention concerns a reflector and a satellite antenna system comprising such a reflector. In the satellite antenna system, microwave radiation from one or more feed horns (5) is emitted at the reflector (1), which comprises first and second reflector elements (2, 3). Upon reflection of the radiation from the reflector elements (2, 3), a distinct beam shape for the reflected microwave energy is generated. The reflector elements (2, 3) are disposed at a fixed distance from one another so that radiation that passes the first reflector element (2) strikes the second element. The first reflector element (2) comprises a lattice structure aimed toward the feed horn, which lattice structure consists of plates (8) of electrically conductive material, wherein the distance between the plates and the depth of said plates are adapted for reflection of polarization parallel to the plates. The invention is characterized in that the extent of each respective plate toward the second reflector element is chosen so that the transmission losses in the first reflector element are minimized.
    • 本发明涉及一种包括这种反射器的反射器和卫星天线系统。 在卫星天线系统中,来自一个或多个馈电喇叭(5)的微波辐射在包括第一和第二反射器元件(2,3)的反射器(1)处发射。 在反射来自反射器元件(2,3)的辐射时,产生用于反射的微波能量的不同的光束形状。 反射器元件(2,3)以彼此固定的距离设置,使得穿过第一反射器元件(2)的辐射撞击第二元件。 第一反射器元件(2)包括针对馈电喇叭的格子结构,该格子结构由导电材料的板(8)组成,其中板之间的距离和所述板的深度适于反射偏振平行 到盘子 本发明的特征在于,朝向第二反射器元件的每个相应板的范围被选择为使得第一反射器元件中的传输损耗最小化。
    • 7. 发明申请
    • COUPLING FOR A SPACE VESSEL
    • 空运船联系
    • WO2003033349A1
    • 2003-04-24
    • PCT/SE2002/001801
    • 2002-10-03
    • SAAB ERICSSON SPACE ABANDERSSON, Torbjörn
    • ANDERSSON, Torbjörn
    • B64G1/64
    • B64G1/641B64G1/002
    • The invention concerns a coupling 4 for a space vessel 1 for holding together a vessel part 2 and a protective envelope 3 that is separable from the vessel part 2. The coupling comprises a first outer flange 5 that is arranged on the vessel part 2, and a second outer flange 6 that is arranged on the protective envelope. The coupling further comprises a number of clamps 7, which are distributed along the periphery of the flanges 5, 6 to transfer radial forces from a tension element that surrounds the clamps 5, 6. The outer flanges are joined by the combination of clamps and tension elements. The coupling further comprises a radially inwardly oriented second inner flange 11, which is arranged on the vessel part 2. The first inner flange 9 is integrally realized with at least one surrounding element 10, which surrounds the second inner flange 11 at least partly.
    • 本发明涉及用于将容器部分2和可与容器部分2分离的保护性外壳3保持在一起的用于空间容器1的联接器4.联接器包括布置在容器部分2上的第一外凸缘5和 布置在保护外壳上的第二外凸缘6。 联接器还包括多个夹具7,其沿着凸缘5,6的周边分布,以从包围夹具5,6的张力元件传递径向力。外凸缘通过夹具和张力的组合 元素。 联接器还包括设置在容器部分2上的径向向内定向的第二内凸缘11.第一内凸缘9与至少一个围绕第二内凸缘11至少部分的周围元件10一体地实现。